12806 Federal Register / Vol. 81, No. 48 / Friday, March 11, 2016 / Rules and Regulations 

(f) Alternative Methods of Compliance 

(AMOCs) 

(1) The Manager, Safety Management 

Group, FAA, may approve AMOCs for this 

AD. Send your proposal to: David Hatfield, 

Aviation Safety Engineer, Safety Management 

Group, Rotorcraft Directorate, FAA, 10101 

Hillwood Pkwy, Fort Worth, TX 76177; 

telephone (817) 222–5116; email 9-ASWFTW-AMOC-Requests@faa.gov. 

(2) For operations conducted under a 14 

CFR part 119 operating certificate or under 

14 CFR part 91, subpart K, we suggest that 

you notify your principal inspector, or 

lacking a principal inspector, the manager of 

the local flight standards district office or 

certificate holding district office, before 

operating any aircraft complying with this 

AD through an AMOC. 

(g) Additional Information 

The subject of this AD is addressed in 

European Aviation Safety Agency (EASA) AD 

No. 2015–0048, dated March 17, 2015. You 

may view the EASA AD on the Internet at 

http://www.regulations.gov by searching for 

and locating it in Docket No. FAA–2015– 

4381. 

(h) Subject 

Joint Aircraft Service Component (JASC) 

Code: Life Raft, 2564. 

(i) Material Incorporated by Reference 

(1) The Director of the Federal Register 

approved the incorporation by reference of 

the service information listed in this 

paragraph under 5 U.S.C. 552(a) and 1 CFR 

part 51. 

(2) You must use this service information 

as applicable to do the actions required by 

this AD, unless the AD specifies otherwise. 

(i) Airbus Helicopters Alert Service 

Bulletin No. AS365–25.01.45, Revision 1, 

dated February 2, 2015. 

(ii) Airbus Helicopters Alert Service 

Bulletin No. EC155–25A128, Revision 1, 

dated February 2, 2015. 

(3) For Airbus Helicopters service 

information identified in this final rule, 

contact Airbus Helicopters, 2701 N. Forum 

Drive, Grand Prairie, TX 75052; telephone 

(972) 641–0000 or (800) 232–0323; fax (972) 

641–3775; or at http://

www.airbushelicopters.com/techpub. 

(4) You may view this service information 

at FAA, Office of the Regional Counsel, 

Southwest Region, 10101 Hillwood Pkwy, 

Room 6N–321, Fort Worth, TX 76177. For 

information on the availability of this 

material at the FAA, call (817) 222–5110. 

(5) You may view this service information 

that is incorporated by reference at the 

National Archives and Records 

Administration (NARA). For information on 

the availability of this material at NARA, call 

(202) 741–6030, or go to: http://

www.archives.gov/federal-register/cfr/ibrlocations.html. 

Issued in Fort Worth, Texas, on February 

29, 2016. 

Scott A. Horn, 

Acting Manager, Rotorcraft Directorate, 

Aircraft Certification Service. 

[FR Doc. 2016–04981 Filed 3–10–16; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2015–0248; Directorate 

Identifier 2014–NM–143–AD; Amendment 

39–18410; AD 2016–04–16] 

RIN 2120–AA64 

Airworthiness Directives; The Boeing 

Company Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: We are superseding 

Airworthiness Directive (AD) 2013–08– 

23 for all The Boeing Company Model 

DC–10–10, DC–10–10F, DC–10–15, DC– 

10–30, DC–10–30F (KC–10A and KDC– 

10), DC–10–40, DC–10–40F, MD–10– 

10F, MD–10–30F, MD–11, and MD–11F 

airplanes. AD 2013–08–23 required 

adding design features to detect 

electrical faults and to detect a pump 

running in an empty fuel tank. This new 

AD would clarify certain requirements 

and remove a terminating action. This 

new AD would also provide an optional 

method of compliance for the proposed 

actions. This AD was prompted by a 

determination that it is necessary to 

clarify the requirements for the design 

features and to remove a terminating 

action for certain inspections. We are 

issuing this AD to reduce the potential 

of ignition sources inside fuel tanks, 

which, in combination with flammable 

fuel vapors, could result in fuel tank 

explosions and consequent loss of the 

airplane. 

DATES: This AD is effective April 15, 

2016. 

The Director of the Federal Register 

approved the incorporation by reference 

of certain publications listed in this AD 

as of April 15, 2016. 

ADDRESSES: For service information 

identified in this final rule, contact 

Boeing Commercial Airplanes, 

Attention: Data & Services Management, 

3855 Lakewood Boulevard, MC D800– 

0019, Long Beach, CA 90846–0001; 

telephone 206–544–5000, extension 2; 

fax 206–766–5683; Internet https://

www.myboeingfleet.com. You may view 

this referenced service information at 

the FAA, Transport Airplane 

Directorate, 1601 Lind Avenue SW., 

Renton, WA. For information on the 

availability of this material at the FAA, 

call 425–227–1221. It is also available 

on the Internet at http://

www.regulations.gov by searching for 

and locating Docket No. FAA–2015– 

0248. 

Examining the AD Docket 

You may examine the AD docket on 

the Internet at http://

www.regulations.gov by searching for 

and locating Docket No. FAA–2015– 

0248; or in person at the Docket 

Management Facility between 9 a.m. 

and 5 p.m., Monday through Friday, 

except Federal holidays. The AD docket 

contains this AD, the regulatory 

evaluation, any comments received, and 

other information. The address for the 

Docket Office (phone: 800–647–5527) is 

Docket Management Facility, U.S. 

Department of Transportation, Docket 

Operations, M–30, West Building 

Ground Floor, Room W12–140, 1200 

New Jersey Avenue SE., Washington, 

DC 20590. 

FOR FURTHER INFORMATION CONTACT: Serj 

Harutunian, Aerospace Engineer, 

Propulsion Branch, ANM–140L, FAA, 

Los Angeles Aircraft Certification Office 

(ACO), 3960 Paramount Boulevard, 

Lakewood, CA 90712–4137; phone: 

562–627–5254; fax: 562–627–5210; 

email: serj.harutunian@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Discussion 

We issued a notice of proposed 

rulemaking (NPRM) to amend 14 CFR 

part 39 to supersede AD 2013–08–23, 

Amendment 39–17441 (78 FR 24037, 

April 24, 2013). AD 2013–08–23 applied 

to all The Boeing Company Model DC– 

10–10, DC–10–10F, DC–10–15, DC–10– 

30, DC–10–30F (KC–10A and KDC–10), 

DC–10–40, DC–10–40F, MD–10–10F, 

MD–10–30F, MD–11, and MD–11F 

airplanes. The NPRM published in the 

Federal Register on March 27, 2015 (80 

FR 16321). The NPRM was prompted by 

a determination that it is necessary to 

clarify the requirements for the design 

features and to remove a terminating 

action for certain inspections. The 

NPRM proposed to clarify certain 

requirements and remove a terminating 

action. The NPRM also proposed to 

provide an optional method of 

compliance for the proposed actions. 

We are issuing this AD to reduce the 

potential of ignition sources inside fuel 

tanks, which, in combination with 

flammable fuel vapors, could result in 

fuel tank explosions and consequent 

loss of the airplane. 

Comments 

We gave the public the opportunity to 

participate in developing this AD. The 

following presents the comments 

received on the NPRM (80 FR 16321, 

March 27, 2015) and the FAA’s response 

to each comment. 


asabaliauskas on DSK3SPTVN1PROD with RULES
Federal Register / Vol. 81, No. 48 / Friday, March 11, 2016 / Rules and Regulations 12807 

Support for the NPRM (80 FR 16321, 

March 27, 2015) 

Boeing stated that it supports the 

NPRM (80 FR 16321, March 27, 2015). 

Request for Clarification 

FedEx requested that we clarify 

paragraph (h)(3) of the proposed AD (80 

FR 16321, March 27, 2015) because it is 

unclear and confusing. 

FedEx explained that paragraphs 

(h)(1) and (h)(2) of the proposed AD (80 

FR 16321, March 27, 2015) propose to 

mandate compliance with Boeing Alert 

Service Bulletin MD11–28A133, dated 

June 5, 2014; Boeing Service Bulletin 

MD11–28–137, dated June 24, 2014; 

Boeing Alert Service Bulletin DC10– 

28A253, dated June 5, 2014; and Boeing 

Service Bulletin DC10–28–256, dated 

June 24, 2014. This service information, 

in addition to describing procedures for 

airframe modifications, specifies 

revising Airworthiness Limitation 

Instructions (ALI) 28–1, Trijet Fuel 

Pump Fault Current Detector Functional 

Check; ALI 28–2, DC–10/KDC–10 

Uncommanded On Circuit Functional 

Check; ALI 28–3, MD–10 

Uncommanded On Circuit Functional 

Check; and ALI 28–4, MD–11 

Uncommanded On Circuit Functional 

Check, Boeing Trijet Special 

Compliance Item Report MDC–02K1003, 

Revision M, dated July 25, 2014. FedEx 

stated that paragraph (h)(3) of the 

proposed AD creates confusion because 

Appendixes B and C of Boeing Trijet 

Special Compliance Item Report MDC– 

02K1003, Revision M, dated July 25, 

2014, also change/affect Critical Design 

Configuration Control Limitation 

(CDCCL) 20–9, Trijet Wing Root Area 

Lightning Protection, (Boeing Service 

Bulletin DC10–28–262, Revision 1, 

dated June 9, 2010, which was 

mandated by AD 2010–21–13, 

Amendment 39–16473 (75 FR 63040, 

October 14, 2010), and has nothing to do 

with the intent of this NPRM, which 

supersedes AD 2013–08–23, 

Amendment 39–17441 (78 FR 24037, 

April 24, 2013). 

FedEx also noted that paragraph (h)(3) 

of the proposed AD (80 FR 16321, 

March 27, 2015) states that revising the 

maintenance or inspection program 

terminates the requirements in 

paragraphs (g) and (h) of AD 2008–06– 

21 R1, Amendment 39–16100 (74 FR 

61504, November 25, 2009). FedEx 

requested that we identify the 

requirements in AD 2008–06–21 R1 that 

would be terminated. FedEx reasoned 

that paragraphs (g) and (h) of AD 2008– 

06–21 R1 cannot be terminated because 

CDCCLs and ALIs are constantly revised 

or new items added to meet safety 

requirements, so latent failures must be 

addressed in the fuel system design. 

We agree that clarification is 

necessary. AD 2010–21–13, Amendment 

39–16473 (75 FR 63040, October 14, 

2010), requires installing a support 

bracket and coupler on the left and right 

wing-to-fuselage transition, and metallic 

overbraid on the left and right leading 

edge wire assembly but it does not 

require revising the maintenance or 

inspection program to incorporate a 

corresponding CDCCL. Paragraph (h)(3) 

of this AD includes incorporating 

CDCCL 20–9, Trijet Wing Root Area 

Lightning Protection, as part of the 

maintenance or inspection program. 

Notwithstanding any other maintenance 

or operational requirements, 

components that have been identified as 

airworthy or installed on the affected 

airplanes before accomplishing the 

revision of the airplane maintenance or 

inspection program specified in this AD, 

do not need to be reworked in 

accordance with the CDCCLs. However, 

once the airplane maintenance or 

inspection program has been revised as 

required by this AD, future maintenance 

actions on these components must be 

done in accordance with the CDCCLs. 

In regards to FedEx’s comment on 

terminating action, we note that AD 

2008–06–21 R1, Amendment 39–16100 

(74 FR 61504, November 25, 2009) 

requires incorporation of Boeing Trijet 

Special Compliance Item Report, MDC– 

02K1003, Revision C, dated July 24, 

2007. Paragraph (h)(3) of this AD 

requires a revision of the maintenance 

or inspection program to include Boeing 

Trijet Special Compliance Item (SCI) 

Report MDC–02K1003, Revision M, 

dated July 25, 2014. We are requiring 

the actions specified in Appendixes B, 

C, and D of Boeing Trijet Special 

Compliance Item Report MDC–02K1003, 

Revision M, dated July 25, 2014, 

because they include the latest CDCCLs, 

ALIs, and short-term extensions. 

Therefore, accomplishing the revision 

required by paragraph (h)(3) of this AD 

would terminate the requirements in 

paragraphs (g) and (h) of AD 2008–06– 

21 R1. Accomplishing paragraph (h)(3) 

of this AD would replace the existing 

requirements with updated 

requirements. We have not changed this 

AD in this regard. 

Conclusion 

We reviewed the relevant data, 

considered the comments received, and 

determined that air safety and the 

public interest require adopting this AD 

as proposed, except for minor editorial 

changes. We have determined that these 

minor changes: 

• Are consistent with the intent that 

was proposed in the NPRM (80 FR 

16321, March 27, 2015) for correcting 

the unsafe condition; and 

• Do not add any additional burden 

upon the public than was already 

proposed in the NPRM (80 FR 16321, 

March 27, 2015). 

We also determined that these 

changes will not increase the economic 

burden on any operator or increase the 

scope of this AD. 

Related Service Information Under 

1 CFR Part 51 

We reviewed the following service 

information. 

• Boeing Alert Service Bulletin 

DC10–28A253, dated June 5, 2014; and 

Boeing Alert Service Bulletin MD11– 

28A133, dated June 5, 2014. This 

service information describes 

procedures for replacing the fuel pump 

control relays with fault current 

detectors and changing the fuel tank 

boost/transfer pump wire termination. 

• Boeing Service Bulletin DC10–28– 

256, dated June 24, 2014; and Boeing 

Service Bulletin MD11–28–137, dated 

June 24, 2014; which describe 

procedures for changing the fuel pump 

control and indication system wiring. 

• Boeing Trijet Special Compliance 

Item Report MDC–02K1003, Revision M, 

including Appendices A through D, 

dated July 25, 2014, which includes 

CDCCLs, ALIs, and short-term 

extensions in Appendices B, C, and D, 

respectively. 

This service information is reasonably 

available because the interested parties 

have access to it through their normal 

course of business or by the means 

identified in the ADDRESSES section. 

Costs of Compliance 

We estimate that this AD affects 341 

airplanes of U.S. registry. 

We estimate the following costs to 

comply with this AD: 


asabaliauskas on DSK3SPTVN1PROD with RULES
12808 Federal Register / Vol. 81, No. 48 / Friday, March 11, 2016 / Rules and Regulations 

ESTIMATED COSTS

Action Labor cost Parts cost Cost per 

product 

Cost on U.S. 

operators 

Installing design features using a method approved by the 

FAA [retained action from AD 2013-08-23, Amendment 

39-17441 (78 FR 24037, April 24, 2013)].

152 work-hours × $85 per 

hour = $12,920.

$137,500 $150,420 $51,923,220 

Installing design features using service information specified 

in paragraph (h) of this AD (including revising the maintenance/inspection program) [new option of this AD].

98 work-hours × $85 per hour 

= $8,330.

109,000 117,330 40,009,530 

Authority for This Rulemaking 

Title 49 of the United States Code 

specifies the FAA’s authority to issue 

rules on aviation safety. Subtitle I, 

Section 106, describes the authority of 

the FAA Administrator. Subtitle VII, 

Aviation Programs, describes in more 

detail the scope of the Agency’s 

authority. 

We are issuing this rulemaking under 

the authority described in Subtitle VII, 

Part A, Subpart III, Section 44701, 

‘‘General requirements.’’ Under that 

section, Congress charges the FAA with 

promoting safe flight of civil aircraft in 

air commerce by prescribing regulations 

for practices, methods, and procedures 

the Administrator finds necessary for 

safety in air commerce. This regulation 

is within the scope of that authority 

because it addresses an unsafe condition 

that is likely to exist or develop on 

products identified in this rulemaking 

action. 

Regulatory Findings 

We have determined that this AD will 

not have federalism implications under 

Executive Order 13132. This AD will 

not have a substantial direct effect on 

the States, on the relationship between 

the national government and the States, 

or on the distribution of power and 

responsibilities among the various 

levels of government. 

For the reasons discussed above, I 

certify that this AD: 

(1) Is not a ‘‘significant regulatory 

action’’ under Executive Order 12866, 

(2) Is not a ‘‘significant rule’’ under 

DOT Regulatory Policies and Procedures 

(44 FR 11034, February 26, 1979), 

(3) Will not affect intrastate aviation 

in Alaska, and 

(4) Will not have a significant 

economic impact, positive or negative, 

on a substantial number of small entities 

under the criteria of the Regulatory 

Flexibility Act. 

List of Subjects in 14 CFR Part 39 

Air transportation, Aircraft, Aviation 

safety, Incorporation by reference, 

Safety. 

Adoption of the Amendment 

Accordingly, under the authority 

delegated to me by the Administrator, 

the FAA amends 14 CFR part 39 as 

follows: 

PART 39—AIRWORTHINESS 

DIRECTIVES 

■ 1. The authority citation for part 39 

continues to read as follows: 

Authority: 49 U.S.C. 106(g), 40113, 44701. 

§ 39.13 [Amended] 

■ 2. The FAA amends § 39.13 by 

removing Airworthiness Directive (AD) 

2013–08–23, Amendment 39–17441 (78 

FR 24037, April 24, 2013), and adding 

the following new AD: 

2016–04–16 The Boeing Company: 

Amendment 39–18410; Docket No. 

FAA–2015–0248; Directorate Identifier 

2014–NM–143–AD. 

(a) Effective Date 

This AD is effective April 15, 2016. 

(b) Affected ADs 

(1) This AD replaces AD 2013–08–23, 

Amendment 39–17441 (78 FR 24037, April 

24, 2013). 

(2) This AD affects AD 2008–06–21 R1, 

Amendment 39–16100 (74 FR 61504, 

November 25, 2009). 

(3) This AD affects AD 2002–13–10, 

Amendment 39–12798 (67 FR 45053, July 8, 

2002). 

(4) This AD affects AD 2011–11–05, 

Amendment 39–16704 (76 FR 31462, June 1, 

2011). 

(c) Applicability 

This AD applies to all The Boeing 

Company airplanes identified in paragraphs 

(c)(1) and (c)(2) of this AD, certificated in any 

category. 

(1) Model DC–10–10, DC–10–10F, DC–10– 

15, DC–10–30, DC–10–30F (KC–10A and 

KDC–10), DC–10–40, DC–10–40F airplanes. 

(2) Model MD–10–10F, MD–10–30F, MD– 

11, and MD–11F airplanes. 

(d) Subject 

Air Transport Association (ATA) of 

America Code 28, Fuel. 

(e) Unsafe Condition 

This AD was prompted by a fuel system 

review conducted by the manufacturer. We 

are issuing this AD to reduce the potential of 

ignition sources inside fuel tanks, which, in 

combination with flammable fuel vapors, 

could result in fuel tank explosions and 

consequent loss of the airplane. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Retained Criteria for Operation, With 

Clarifications and New Compliance Time 

This paragraph restates the actions 

required by paragraph (g) of AD 2013–08–23, 

Amendment 39–17441 (78 FR 24037, April 

24, 2013), with clarification of actions for 

airplanes with auxiliary fuel tanks removed, 

clarification of the pumps that must have a 

protective device installed, and a new 

compliance time. Except as provided by 

paragraph (h) of this AD: As of 48 months 

after the effective date of this AD, no person 

may operate any airplane affected by this AD 

unless an amended type certificate or 

supplemental type certificate that 

incorporates the design features and 

requirements described in paragraphs (g)(1) 

through (g)(4) of this AD has been approved 

by the Manager, Los Angeles Aircraft 

Certification Office (ACO), FAA, and those 

design features are installed on the airplane 

to meet the criteria specified in section 

25.981(a) and (d) of the Federal Aviation 

Regulations (14 CFR 25.981(a) and (d), at 

Amendment 25–125 (http://rgl.faa.gov/

Regulatory_and_Guidance_Library/

rgFAR.nsf/0/339DAEE3E0A6379D862574C

F00641951?OpenDocument)). For airplanes 

on which Boeing-installed auxiliary fuel 

tanks are removed, the actions specified in 

this AD for the auxiliary fuel tanks are not 

required. 

(1) For all airplanes: Each electrically 

powered alternating current (AC) fuel pump 

installed in any fuel tank that normally 

empties during flight and each pump that is 

partially covered by a lowering fuel level— 

such as main tanks, center wing tanks, 

auxiliary fuel tanks installed by the airplane 

manufacturer, and tail tanks—must have a 

protective device installed to detect electrical 

faults that can cause arcing and burn through 

of the fuel pump housing and pump 

electrical connector. The same device must 

shut off the pump by automatically removing 

electrical power from the pump when such 

faults are detected. When a fuel pump is shut 

off resulting from detection of an electrical 

fault, the device must stay latched off, until 

the fault is cleared through maintenance 

action and the pump is verified safe for 

operation. 


asabaliauskas on DSK3SPTVN1PROD with RULES
Federal Register / Vol. 81, No. 48 / Friday, March 11, 2016 / Rules and Regulations 12809 

(2) For airplanes with a 2-person 

flightcrew: Additional design features, if not 

originally installed by the airplane 

manufacturer, must be installed to meet 3 

criteria: To detect a running fuel pump in a 

tank that is normally emptied during flight, 

to provide an indication to the flightcrew that 

the tank is empty, and to automatically shut 

off that fuel pump. The prospective pump 

indication and shutoff system must 

automatically shut off each pump in case the 

flightcrew does not shut off a pump running 

dry in an empty tank within 60 seconds after 

each fuel tank is emptied. An airplane flight 

manual supplement (AFMS) that includes 

flightcrew manual pump shutoff procedures 

in the Limitations section of the AFMS must 

be submitted to the Los Angeles ACO, FAA, 

for approval. 

(3) For airplanes with a 3-person 

flightcrew: Additional design features, if not 

originally installed by the airplane 

manufacturer, must be installed to detect 

when a fuel pump in a tank that is normally 

emptied during flight is running in an empty 

fuel tank, and to provide an indication to the 

flightcrew that the tank is empty. The flight 

engineer must manually shut off each pump 

running dry in an empty tank within 60 

seconds after the tank is emptied. The AFMS 

Limitations section must be revised to 

specify that this pump shutoff must be done 

by the flight engineer. 

(4) For all airplanes with tanks that 

normally empty during flight: Separate 

means must be provided to detect and shut 

off a pump that was previously commanded 

to be shut off automatically or manually but 

remained running in an empty tank during 

flight. 

(h) New Optional Method of Compliance 

In lieu of doing the requirements of 

paragraph (g) of this AD, do the applicable 

actions specified in paragraphs (h)(1), (h)(2), 

and (h)(3) of this AD. 

(1) For MD–11 and MD–11F airplanes: Do 

the actions specified in paragraphs (h)(1)(i) 

and (h)(1)(ii) of this AD. 

(i) As of 48 months after the effective date 

of this AD, change the fuel pump control and 

indication system wiring, in accordance with 

the Accomplishment Instructions of Boeing 

Service Bulletin MD11–28–137, dated June 

24, 2014. 

(ii) Prior to or concurrently with 

accomplishing the actions specified in 

paragraph (h)(1)(i) of this AD: Replace the 

fuel pump control relays with fault current 

detectors, and change the fuel tank boost/

transfer pump wire termination, in 

accordance with Accomplishment 

Instructions of Boeing Alert Service Bulletin 

MD11–28A133, dated June 5, 2014. 

(2) For Model DC–10–10, DC–10–10F, DC– 

10–15, DC–10–30, DC–10–30F (KC–10A and 

KDC–10), DC–10–40, DC–10–40F, MD–10– 

10F, and MD–10–30F airplanes: Do the 

actions specified in paragraphs (h)(2)(i) and 

(h)(2)(ii) of this AD. 

(i) As of 48 months after the effective date 

of this AD, change the fuel pump control and 

indication system wiring, in accordance with 

the Accomplishment Instructions of Boeing 

Service Bulletin DC10–28–256, dated June 

24, 2014. 

(ii) Prior to or concurrently with 

accomplishing the actions specified in 

paragraph (h)(2)(i) of this AD: Replace the 

fuel pump control relays with fault current 

detectors, and change the fuel tank boost/

transfer pump wire termination, in 

accordance with the Accomplishment 

Instructions of Boeing Alert Service Bulletin 

DC10–28A253, dated June 5, 2014. 

(3) For all airplanes: Within 30 days after 

accomplishing the actions required by 

paragraph (h)(1) or (h)(2) of this AD, or 

within 30 days after the effective date of this 

AD, whichever occurs later, revise the 

maintenance or inspection program, as 

applicable, to incorporate the Critical Design 

Configuration Control Limitations (CDCCLs), 

Airworthiness Limitation Instructions (ALIs), 

and short-term extensions specified in 

Appendices B, C, and D of Boeing Trijet 

Special Compliance Item (SCI) Report MDC– 

02K1003, Revision M, dated July 25, 2014. 

The initial compliance time for 

accomplishing the actions specified in the 

ALIs is at the later of the times specified in 

paragraphs (h)(3)(i) and (h)(3)(ii) of this AD. 

Revising the maintenance or inspection 

program required by this paragraph 

terminates the requirements in paragraphs (g) 

and (h) of AD 2008–06–21 R1, Amendment 

39–16100 (74 FR 61504, November 25, 2009). 

(i) At the applicable time specified in 

Appendix C of Boeing Trijet SCI Report 

MDC–02K1003, Revision M, dated July 25, 

2014, except as provided by Appendix D of 

Boeing Trijet SCI Report MDC–02K1003, 

Revision M, dated July 25, 2014. 

(ii) Within 30 days after accomplishing the 

actions required by paragraph (h)(1) or (h)(2) 

of this AD, as applicable; or within 30 days 

after the effective date of this AD; whichever 

occurs later. 

(i) No Alternative Actions, Intervals, or 

CDCCLs 

If the option in paragraph (h)(3) of this AD 

is accomplished: After the maintenance or 

inspection program has been revised as 

provided by paragraph (h)(3) of this AD, no 

alternative actions (e.g., inspections), 

intervals, or CDCCLs may be used unless the 

actions, intervals, or CDCCLs are approved as 

an alternative method of compliance (AMOC) 

in accordance with the procedures specified 

in paragraph (k) of this AD. 

(j) Compliance Time Extension in Related 

ADs 

Accomplishment of the actions specified in 

paragraphs (h)(1), (h)(2), and (h)(3) of this 

AD, as applicable, extends the 18-month 

repetitive inspections and tests required by 

paragraph (a) of AD 2002–13–10, 

Amendment 39–12798 (67 FR 45053, July 8, 

2002); and the 18-month repetitive 

inspections required by paragraph (j) of AD 

2011–11–05, Amendment 39–16704 (76 FR 

31462, June 1, 2011); to 24-month intervals 

for pumps affected by those ADs, regardless 

if the pump is installed in a tank that 

normally empties, provided the remaining 

actions required by those two ADs have been 

accomplished. 

(k) Alternative Methods of Compliance 

(AMOCs) 

(1) The Manager, Los Angeles ACO, FAA, 

has the authority to approve AMOCs for this 

AD, if requested using the procedures found 

in 14 CFR 39.19. In accordance with 14 CFR 

39.19, send your request to your principal 

inspector or local Flight Standards District 

Office, as appropriate. If sending information 

directly to the manager of the ACO, send it 

to the attention of the person identified in 

paragraph (l) of this AD. Information may be 

emailed to: 9-ANM-LAACO-AMOCRequests@faa.gov. 

(2) Before using any approved AMOC, 

notify your appropriate principal inspector, 

or lacking a principal inspector, the manager 

of the local flight standards district office/

certificate holding district office. 

(3) An AMOC that provides an acceptable 

level of safety may be used for any repair 

required by this AD if it is approved by the 

Boeing Commercial Airplanes Organization 

Designation Authorization (ODA) that has 

been authorized by the Manager, Los Angeles 

ACO, to make those findings. For a repair 

method to be approved, the repair must meet 

the certification basis of the airplane, and the 

approval must specifically refer to this AD. 

(4) AMOCs approved for AD 2013–08–23, 

Amendment 39–17441 (78 FR 24037, April 

24, 2013), are approved as AMOCs for the 

corresponding provisions of this AD. 

(l) Related Information 

For more information about this AD, 

contact Serj Harutunian, Aerospace Engineer, 

Propulsion Branch, ANM–140L, FAA, Los 

Angeles ACO, 3960 Paramount Boulevard, 

Lakewood, CA 90712–4137; phone: 562–627– 

5254; fax: 562–627–5210; email: 

serj.harutunian@faa.gov. 

(m) Material Incorporated by Reference 

(1) The Director of the Federal Register 

approved the incorporation by reference 

(IBR) of the service information listed in this 

paragraph under 5 U.S.C. 552(a) and 1 CFR 

part 51. 

(2) You must use this service information 

as applicable to do the actions required by 

this AD, unless the AD specifies otherwise. 

(i) Boeing Alert Service Bulletin DC10– 

28A253, dated June 5, 2014. 

(ii) Boeing Alert Service Bulletin MD11– 

28A133, dated June 5, 2014. 

(iii) Boeing Service Bulletin DC10–28–256, 

dated June 24, 2014. 

(iv) Boeing Service Bulletin MD11–28–137, 

dated June 24, 2014. 

(v) Boeing Trijet Special Compliance Item 

Report MDC–02K1003, Revision M, 

including Appendices A through D, dated 

July 25, 2014. 

(3) For Boeing service information 

identified in this AD, contact Boeing 

Commercial Airplanes, Attention: Data & 

Services Management, 3855 Lakewood 

Boulevard, MC D800–0019, Long Beach, CA 

90846–0001; telephone 206–544–5000, 

extension 2; fax 206–766–5683; Internet 

https://www.myboeingfleet.com. 

(4) You may view this service information 

at FAA, Transport Airplane Directorate, 1601 

Lind Avenue SW., Renton, WA. For 

information on the availability of this 

material at the FAA, call 425–227–1221. 


asabaliauskas on DSK3SPTVN1PROD with RULES
12810 Federal Register / Vol. 81, No. 48 / Friday, March 11, 2016 / Rules and Regulations 

(5) You may view this service information 

that is incorporated by reference at the 

National Archives and Records 

Administration (NARA). For information on 

the availability of this material at NARA, call 

202–741–6030, or go to: http://

www.archives.gov/federal-register/cfr/ibrlocations.html. 

Issued in Renton, Washington, on February 

8, 2016. 

Michael Kaszycki, 

Acting Manager, Transport Airplane 

Directorate, Aircraft Certification Service. 

[FR Doc. 2016–04564 Filed 3–10–16; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 71 

[Docket No. FAA–2015–7489; Airspace 

Docket No. 15–ASW–20] 

Amendment of Class D and E 

Airspace; Enid Vance AFB, OK; Enid 

Woodring Municipal Airport, Enid, OK; 

and Enid, OK 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule; delay of effective 

date, correction. 

SUMMARY: This action changes the 

effective date of a final rule published 

in the Federal Register of February 19, 

2016, amending Class E surface area 

airspace, Class E airspace designated as 

an extension, and Class E airspace 

extending upward from 700 feet above 

the surface, in the Enid, OK, area to 

allow additional time for charting. This 

correction adds the part-time Notice to 

Airmen (NOTAM) language 

inadvertently removed from the Class E 

surface area description for Vance AFB, 

and Woodring Municipal Airport, Enid, 

OK. Adjustment of the geographic 

coordinates are also made to the Vance 

VHF Omnidirectional Range Tactical 

Air Navigation (VORTAC) listed in the 

Class E airspace area designated as an 

extension to the Class D surface area. 

DATES: This correction is effective 0901 

UTC, July 21, 2016, and the effective 

date of the rule amending 14 CFR part 

71 published on February 19, 2016 (81 

FR 8389), is delayed to 0901 UTC July 

21, 2016. 

The Director of the Federal Register 

approves this incorporation by reference 

action under Title 1, Code of Federal 

Regulations, part 51, subject to the 

annual revision of FAA Order 7400.9 

and publication of conforming 

amendments. 

FOR FURTHER INFORMATION CONTACT: 

Jeffrey Claypool, Federal Aviation 

Administration, Operations Support 

Group, Central Service Center, 10101 

Hillwood Parkway, Fort Worth, TX, 

76177; telephone (817) 222–5711. 

SUPPLEMENTARY INFORMATION: 

History 

The Federal Register published a 

final rule amending Class E surface area 

airspace, Class E airspace designated as 

an extension, and Class E airspace 

extending upward from 700 feet above 

the surface, at Vance AFB, Enid, OK; 

and Woodring Municipal Airport, Enid, 

OK (81 FR 8389, February 19, 2016) 

Docket No. FAA–2015–7489. 

Subsequent to publication, the FAA 

determined that the part-time NOTAM 

language in the Class E surface area 

description was inadvertently removed 

in error. Potential safety concerns were 

identified due to the possibility for 

confusion in determining the operating 

rules and equipment requirements in 

the Vance AFB and Woodring 

Municipal Airport terminal areas. The 

concerns were based on the opportunity 

for part-time Class D surface area 

airspace and continuous Class E surface 

area airspace to be active at the same 

time. 

To resolve these concerns, the FAA is 

keeping the part-time NOTAM language 

in the Class E surface area description 

to retain it as part-time airspace 

supplementing the existing part-time 

Class D surface area airspace at Vance 

AFB and Woodring Municipal Airport. 

The regulatory text is rewritten for 

clarity. A minor adjustment is also made 

to the geographic coordinates of the 

Vance VORTAC listed in Class E 

airspace area designated as an extension 

to Class D. These are administrative 

corrections and do not affect the 

controlled airspace boundaries or 

operating requirements supporting 

operations in the Vance AFB and 

Woodring Municipal Airport terminal 

areas. 

Correction to Final Rule 

Accordingly, pursuant to the 

authority delegated to me, in the 

Federal Register of February 19, 2016 

(81 FR 8389) FR Doc. 2016–03365, 

Amendment of Class D and E Airspace; 

Enid Vance AFB, Ok; Enid Woodring 

Municipal Airport, Enid, OK; and Enid, 

OK, is corrected as follows: 

§ 71.1 [Amended] 

ASW OK E2 Enid, OK [Corrected] 

■ On page 8390, column 3, beginning on 

line 42, remove the following text: 

‘‘Within a 5.1-mile radius of Vance 

AFB, and within a 4.1-mile radius of 

Woodring Municipal Airport.’’, and add 

in its place: 

‘‘Within a 5.1-mile radius of Vance 

AFB, and within a 4.1-mile radius of 

Woodring Municipal Airport. This Class 

E airspace area is effective during the 

specific dates and times established in 

advance by a Notice to Airmen. The 

effective date and time will thereafter be 

continuously published in the Airport/ 

Facility Directory.’’ 

ASW OK E4 Enid Vance AFB, OK 

[Corrected] 

■ On page 8390, column 3, line 54, 

remove ‘‘(lat. 36°20′42′′ N., long. 

97°55′07′′ W.)’’ and add in its place 

‘‘(lat. 36°20′42′′ N., long. 97°55′06′′ W.)’’ 

Issued in Fort Worth, Texas, on March 1, 

2016. 

Vonnie Royal 

Acting Manager, Operations Support Group, 

ATO Central Service Center. 

[FR Doc. 2016–05395 Filed 3–10–16; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF COMMERCE 

Office of the Secretary 

15 CFR Part 19 

[Docket No. 150902806–5806–01] 

RIN 0605–AA40 

Commerce Debt Collection 

AGENCY: Office of the Chief Financial 

Officer and Assistant Secretary for 

Administration, Department of 

Commerce. 

ACTION: Final rule. 

SUMMARY: The Department of Commerce 

(Commerce Department) hereby revises 

its debt collection regulations as a result 

of, and to conform to, an amendment 

made by the Digital Accountability and 

Transparency Act of 2014 (DATA Act). 

Specifically, the law, as amended by the 

DATA Act, requires Commerce 

Department to refer to the Secretary of 

the Treasury all past due, legally 

enforceable nontax debt that are over 

120 days delinquent, including nontax 

debt administered by a third party 

acting as an agent for the Federal 

Government, for purposes of 

administrative offset. These revised debt 

collection regulations also provide 

updated references to the Bureau of the 

Fiscal Service as the agency within the 

Department of the Treasury to which 

Commerce Department refers delinquent 

debts to reflect a reorganization made by 

the Department of the Treasury. 


asabaliauskas on DSK3SPTVN1PROD with RULES